US4617977A - Ceramic casting mould and a method for its manufacture - Google Patents

Ceramic casting mould and a method for its manufacture Download PDF

Info

Publication number
US4617977A
US4617977A US06/509,812 US50981283A US4617977A US 4617977 A US4617977 A US 4617977A US 50981283 A US50981283 A US 50981283A US 4617977 A US4617977 A US 4617977A
Authority
US
United States
Prior art keywords
mould
die
disposable
ceramic
pattern
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
US06/509,812
Inventor
David Mills
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Assigned to ROLLS-ROYCE LIMITED, 65 BUCKINGHAM GATE, LONDON SW1E 6AT, ENGLAND reassignment ROLLS-ROYCE LIMITED, 65 BUCKINGHAM GATE, LONDON SW1E 6AT, ENGLAND ASSIGNMENT OF ASSIGNORS INTEREST. Assignors: MILLS, DAVID
Application granted granted Critical
Publication of US4617977A publication Critical patent/US4617977A/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22CFOUNDRY MOULDING
    • B22C13/00Moulding machines for making moulds or cores of particular shapes
    • B22C13/08Moulding machines for making moulds or cores of particular shapes for shell moulds or shell cores
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22CFOUNDRY MOULDING
    • B22C9/00Moulds or cores; Moulding processes
    • B22C9/02Sand moulds or like moulds for shaped castings
    • B22C9/04Use of lost patterns

Definitions

  • the present invention relates to a ceramic casting mould and a method for its manufacture.
  • a widely used process of making moulds is the lost wax process in which a wax pattern of the article to be made is made and is repeatedly invested with particulate ceramic material until the required mould thickness has been built up.
  • One drawback found with this process is that the repeated investment of the pattern produces a layered structure in the ceramic.
  • Another drawback is that the binder used in the ceramic slurry is invariably silica-based, which limits the overall refractoriness of the shells produced to the extent that distortion occurs at the high temperatures used in casting directionally solidified articles.
  • Moulds made by the injection moulding technique are made in two or more parts to minimise the complexity of the dies used.
  • This has the advantage that they can be inspected easily before casting, but has the disadvantage that the parts have to be clamped or cemented together before pouring of the casting takes place.
  • a plurality of moulds made in parts are held together in an assembly by ceramic covers or a strap encircling the assembly.
  • Another disadvantage is that where a cement is used, the mould parts have to be made with flanges to provide sufficient surface to which the cement can be applied.
  • One object of the present invention is to provide a mould defining a casting cavity and which is of thin-walled seamless, homogeneous construction at least in its casting cavity-defining portions.
  • the term "thin-walled” is meant to include moulds having wall thicknesses of the order of 0.5 mm to 2.0 mm thick.
  • Another object of the present invention is to provide a method for the manufacture of such a mould.
  • the invention as claimed herein fulfils these objects in that it uses as an essential feature of the manufacturing process for the mould, the step of injection moulding a ceramic material around a disposable pattern.
  • the injection moulding step produces a homogeneous mould structure and allows the use of higher strength ceramic materials that have not hitherto been used with the lost wax process.
  • injection into a die enclosing a disposable pattern enables seamless moulds to be produced.
  • This in turn enables the mould walls to be made thinner and by choosing a high strength ceramic material which also has a high thermal conductivity, a significant increase can be achieved in the cooling rate of the mould, which reduces the cost of the casting process, particularly where a directionally solidified article is being produced.
  • the method can be used to produce a mould with an integrally formed core very accurately located in it. This can be achieved if an injection moulded core made from the same material as the ceramic material of the mould and cured into its green state is embedded in the disposable pattern. By this means when the mould is fired, the core and the mould will undergo the same amount of shrinkage so that there will be no relative changes in dimension between the two.
  • the mould is supported on its inner and outer wall surfaces during firing of the ceramic, distortion of the walls of the mould can be minimised.
  • FIGS. 1 to 5 illustrate longitudinal sections through a mould of the present invention at various stages of manufacture
  • FIG. 6 illustrates a mould assembly prepared for firing.
  • FIG. 7 illustrates a longitudinal section through a mould of the present invention showing an alternative embodiment for supporting the outer mould wall during firing.
  • FIG. 1 a die 10 having a cavity 11 in which is positioned a pre-formed alumina core 12.
  • the internal surfaces of the die are shaped to produce an accurate pattern of the article to be cast, in this example, a stator vane for a gas turbine engine.
  • the core is supported adjacent its ends and edges in the die leaving end and edge portions 14 and 15 exposed, so that they will not be encapsulated by the material being injected into the die.
  • the core may be pre-fired, in which case its strength may be such that no additional support is necessary. In the preferred method, however, the core is only cured to its "green” state and is preferably also located against movement or distortion during the injection process by high temperature disposable chaplets 13.
  • high temperature as applied to the chaplets means, as will be seen later, that they must be made from a material which retains its strength during the firing of the ceramic mould and core up to a temperature at which the ceramic has acquired sufficient strength not to require further support. Beyond that temperature, but at a temperature less than the final sintering temperature of the ceramic, the chaplets must burn out of the finished mould.
  • the material used for the chaplets has a shrinkage compatible with that of the ceramic at least up to the self-supporting temperature of the ceramic.
  • One type of material which fulfils all of the these requirements is a phenol formaldehyde thermo-setting resin containing a graphite filler.
  • the next step of the method is the injection of the disposable material into the cavity 11, thereby encapsulating the main bulk of the core 12 and the chaplets 13 to form the pattern, but leaving the end and edge portions 14 and 15 of the core exposed.
  • FIG. 2 shows the pattern 16 after removal from the die 10.
  • the pattern 16 is then placed in a further die 20, shown in FIG. 3, for the final part of the process, which is the injection of the ceramic material to form the mould.
  • the pattern 16 is supported at its ends, but additional high temperature chaplets 22 are provided along its length to prevent any movement during the injection process.
  • Ceramic material is injected into the space 35 defined within the die by the disposable pattern, and once set into its so-called "green" state the mould is removed from the die.
  • all but one of the exposed portions 14 and 15 of the core are painted with a polystyrene paint which burns away during firing of the mould.
  • a polystyrene paint which burns away during firing of the mould.
  • FIG. 4 shows the mould at this stage, and all that remains to be done is to remove the disposable pattern 16 and fire the ceramic and core to produce the finished mould which is shown in FIG. 5.
  • the disposable pattern may be removed by melting, burning, dissolution or in any other suitable manner. Where heat is required to remove it, this step of the process may be carried out as part of the firing step. For reasons to be explained below it is preferable that the pattern be removed in a pre-heating step before the mould is fired.
  • mould walls are thin it is preferable to provide support for them to prevent distortion during the firing step.
  • a preferred manner of doing this is to form as assembly of truncated wedge-shaped spacers, each having a shaped recess in one or both faces thereof into which the moulds are fitted.
  • the recesses are shaped to provide areas of contact at various points along the length of the mould outer surface.
  • the wedge-shaped spacers may be arranged to define a cylindrical or polygonal assembly.
  • FIG. 6 shows such a cylindrical assembly of moulds 24 and spacers 30.
  • the spacers should be made of a material which has a shrinkage rate on firing which is compatible with that of the "green” ceramic, and may be made from the same "green” ceramic material.
  • the firing step is preferably carried out in accordance with the method described in the specification of our copending patent application No. 81,11223, now published as British Application No. 2,096,502, filed Oct. 20, 1982.
  • the cylindrical assembly is bound with a refractory tape which shrinks on heating to a greater degree than the ceramic parts of the assembly.
  • the tape pulls the truncated wedges tightly together causing the side-faces of the spacers to provide good support for the walls of the mould.
  • the ceramic moulds and cores in their green state have a degree of flexibility and, during the early part of the firing step, any distortions will be straightened out by the pressure from the spacers.
  • the graphite spacers will support the walls of the mould from inward distortion until the temperature is reached at which they burn out.
  • the mould is made without a core, however, it is preferable to provide support on the inside of the mould, and this can be done by filling the mould with a non-sintering ceramic powder, for example re-crystallised alumina 34, as shown in FIG. 7, or by supports positioned at different places within the mould cavity.
  • the supports may conveniently be provided by embedding in the disposable pattern, pins made from a high temperature disposable material, for example, the graphite supported resin hereinbefore described. These will remain in place when the disposable material is removed but will burn out before the highest sintering temperature of the ceramic is reached.
  • the ceramic material may be a conventional silica composition or one of the higher strength ceramics, such as alumina or zirconia may be used.
  • the ceramic material is mixed with a resin binder for the injection process.
  • the binder may be a thermo-plastic resin which, on injection into a cold die, sets solid, but which softens again on heating.
  • the disposable pattern may be a conventional wax pattern.
  • thermo-setting resin which is injected into a hot die and cured.
  • Such resins once cured retain their strength during the early part of the firing process and do not soften again.
  • a mixture of the two types of resin may be used provided adequate strength is maintained.
  • the disposable pattern material When using thermosetting resin binders, the disposable pattern material must be capable of withstanding the temperature and pressure during the injection of the ceramic material without deformation, but must be capable of being removed by a relatively simple process, for example, burning, melting or dissolution.
  • a preferred material is a water soluble organic compound, for example, cane sugar which retains adequate strength to beyond 150° C., which is the usual injection temperature of the ceramic using a thermosetting resin binder.
  • the cane sugar contains an inert filler such as mica or slate powder, but preferably a soluble filler is used, for example, ammonium chloride and it may contain effervescing agents. Alternatively some low melting point metal alloys may be used, for example, those tin-zinc alloys sold under the Trade names of CERROBENT or CERROTRUE.
  • the chaplets 22 for supporting the pattern 16 in the die 20 must also withstand the pressure and temperature of the injection process. However, since these spacers span the space 24 into which the ceramic is injected, they are preferably made from the same material as the ceramic material being injected but which has previously been cured to its green state. We have found that during the injection process the ceramic integrates with the pieces of the same material cured to the green state to such an extend that the pieces become absorbed into a homogeneous mass without leaving any areas of weakness. These supports thus become part of the mould itself.
  • the core material need not be alumina but is selected in dependence on the requirements of the casting process. Thus silica or any other known core material may be used.
  • another particular advantage of the invention is that the core and mould can be made from the same ceramic material in the same thermosetting resin binder. When injected hot, the binder cures to the green state which has intermediate strength and some flexibility. The mould with its core and supports can all be fired together at the same temperature and there will be no distortion due to differential thermal expansions or differential shrinkage. Thus the core remains accurately positioned within the final mould.
  • the high temperature chaplets 13 may, as an alternative to the graphite compound, be made from a metal compatible with that being cast, and which can be allowed to dissolve in the casting rather than being burned out as the graphite spacers are.
  • One advantage of the above-described process over the conventional lost wax process is that the ceramic from which the mould is made can be accurately injected to give a very thin homogeneous wall thickness. This enables high heat conductivity to be achieved which speeds up the cooling process after casting.
  • the homogeneous material is of uniform cross-section and is not subject to flaking or cracking as is the conventional invested shell mould. Because of the choice of materials available with this process, a material having the most beneficial combination of strength and thermal conductivity can be chosen depending on the casting process being used.
  • the mould can have a varying wall thickness if desired.
  • a disposable article is made without the core and is supported in a die as described above while ceramic is injected around it.
  • the mould described above may form part of a larger multiple mould assembly made completely by an injection process, thus eliminating the need for the time-consuming lost wax investment process currently used for making multiple moulds for casting aerofoil blades in the aero engine industry.
  • the mould shown in the example described above is open-ended ready for connection to a runner system in such a larger assembly.
  • individual moulds with their own runner and riser systems can also be made by the method of the invention.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Molds, Cores, And Manufacturing Methods Thereof (AREA)

Abstract

The present invention provides a method for manufacturing a thin-walled ceramic casting mould which is particularly suitable for casting directionally solidified articles in which rapid cooling of the cast material is required. The mould is transfer moulded around a disposable pattern material and includes an integral core. The mould has an outer wall thickness of the order of 0.5 mm to 2.0 mm. The mould and core may be made of the same or different ceramic materials chosen for their strength or thermal conductivity. The method further provides for a series of high temperature disposable supports embedded in the disposable pattern material, providing support for the outer wall of the mould during the firing process. The disposable supports are disposed of at a temperature at which the mould has acquired self-supporting strength.

Description

The present invention relates to a ceramic casting mould and a method for its manufacture.
A widely used process of making moulds is the lost wax process in which a wax pattern of the article to be made is made and is repeatedly invested with particulate ceramic material until the required mould thickness has been built up. One drawback found with this process is that the repeated investment of the pattern produces a layered structure in the ceramic. Another drawback is that the binder used in the ceramic slurry is invariably silica-based, which limits the overall refractoriness of the shells produced to the extent that distortion occurs at the high temperatures used in casting directionally solidified articles.
In our U.K. Pat. No. 1,584,367 there is described a mould arrangement for casting metal articles in which each mould is made directly in ceramic material by a transfer moulding technique.
Moulds made by the injection moulding technique, particularly those of complex internal shape, are made in two or more parts to minimise the complexity of the dies used. This has the advantage that they can be inspected easily before casting, but has the disadvantage that the parts have to be clamped or cemented together before pouring of the casting takes place. In the process described in the above mentioned patent, a plurality of moulds made in parts are held together in an assembly by ceramic covers or a strap encircling the assembly. Another disadvantage is that where a cement is used, the mould parts have to be made with flanges to provide sufficient surface to which the cement can be applied.
When casting directionally solidified articles, which term includes single crystal articles, the higher temperatures involved make it desirable to have homogeneous moulds which have no bulky joints, and it is also desirable that the moulds should be strong, thin-walled, and have high thermal conductivity. All of these requirements have hitherto not been achieved simultaneously by either of the above-described known processes for making casting moulds.
One object of the present invention is to provide a mould defining a casting cavity and which is of thin-walled seamless, homogeneous construction at least in its casting cavity-defining portions. The term "thin-walled" is meant to include moulds having wall thicknesses of the order of 0.5 mm to 2.0 mm thick.
Another object of the present invention is to provide a method for the manufacture of such a mould.
The invention as claimed herein fulfils these objects in that it uses as an essential feature of the manufacturing process for the mould, the step of injection moulding a ceramic material around a disposable pattern. The injection moulding step produces a homogeneous mould structure and allows the use of higher strength ceramic materials that have not hitherto been used with the lost wax process. At the same time injection into a die enclosing a disposable pattern enables seamless moulds to be produced. This in turn enables the mould walls to be made thinner and by choosing a high strength ceramic material which also has a high thermal conductivity, a significant increase can be achieved in the cooling rate of the mould, which reduces the cost of the casting process, particularly where a directionally solidified article is being produced.
By including in the method of manufacture some or all of the additional steps claimed, further advantageous results can be achieved. For example, the method can be used to produce a mould with an integrally formed core very accurately located in it. This can be achieved if an injection moulded core made from the same material as the ceramic material of the mould and cured into its green state is embedded in the disposable pattern. By this means when the mould is fired, the core and the mould will undergo the same amount of shrinkage so that there will be no relative changes in dimension between the two.
Further, if the mould is supported on its inner and outer wall surfaces during firing of the ceramic, distortion of the walls of the mould can be minimised.
The invention will now be more particularly described, by way of example only, with reference to the accompanying drawings in which:
FIGS. 1 to 5 illustrate longitudinal sections through a mould of the present invention at various stages of manufacture, and,
FIG. 6 illustrates a mould assembly prepared for firing.
FIG. 7 illustrates a longitudinal section through a mould of the present invention showing an alternative embodiment for supporting the outer mould wall during firing.
Referring now to the drawings, there is shown in FIG. 1 a die 10 having a cavity 11 in which is positioned a pre-formed alumina core 12. The internal surfaces of the die are shaped to produce an accurate pattern of the article to be cast, in this example, a stator vane for a gas turbine engine. The core is supported adjacent its ends and edges in the die leaving end and edge portions 14 and 15 exposed, so that they will not be encapsulated by the material being injected into the die.
The core may be pre-fired, in which case its strength may be such that no additional support is necessary. In the preferred method, however, the core is only cured to its "green" state and is preferably also located against movement or distortion during the injection process by high temperature disposable chaplets 13.
The description "high temperature" as applied to the chaplets means, as will be seen later, that they must be made from a material which retains its strength during the firing of the ceramic mould and core up to a temperature at which the ceramic has acquired sufficient strength not to require further support. Beyond that temperature, but at a temperature less than the final sintering temperature of the ceramic, the chaplets must burn out of the finished mould.
It is also preferable that the material used for the chaplets has a shrinkage compatible with that of the ceramic at least up to the self-supporting temperature of the ceramic. One type of material which fulfils all of the these requirements is a phenol formaldehyde thermo-setting resin containing a graphite filler.
The next step of the method is the injection of the disposable material into the cavity 11, thereby encapsulating the main bulk of the core 12 and the chaplets 13 to form the pattern, but leaving the end and edge portions 14 and 15 of the core exposed. FIG. 2 shows the pattern 16 after removal from the die 10.
The pattern 16 is then placed in a further die 20, shown in FIG. 3, for the final part of the process, which is the injection of the ceramic material to form the mould. The pattern 16 is supported at its ends, but additional high temperature chaplets 22 are provided along its length to prevent any movement during the injection process. Ceramic material is injected into the space 35 defined within the die by the disposable pattern, and once set into its so-called "green" state the mould is removed from the die.
To allow for differential thermal expansions, all but one of the exposed portions 14 and 15 of the core are painted with a polystyrene paint which burns away during firing of the mould. Thus only one of the embedded portions becomes integrally fixed to the mould, the others remaining free to slide.
FIG. 4 shows the mould at this stage, and all that remains to be done is to remove the disposable pattern 16 and fire the ceramic and core to produce the finished mould which is shown in FIG. 5.
Depending on the material used as the disposable pattern, it may be removed by melting, burning, dissolution or in any other suitable manner. Where heat is required to remove it, this step of the process may be carried out as part of the firing step. For reasons to be explained below it is preferable that the pattern be removed in a pre-heating step before the mould is fired.
Because the mould walls are thin it is preferable to provide support for them to prevent distortion during the firing step. A preferred manner of doing this is to form as assembly of truncated wedge-shaped spacers, each having a shaped recess in one or both faces thereof into which the moulds are fitted. The recesses are shaped to provide areas of contact at various points along the length of the mould outer surface. When assembled the wedge-shaped spacers may be arranged to define a cylindrical or polygonal assembly.
FIG. 6 shows such a cylindrical assembly of moulds 24 and spacers 30. The spacers should be made of a material which has a shrinkage rate on firing which is compatible with that of the "green" ceramic, and may be made from the same "green" ceramic material.
The firing step is preferably carried out in accordance with the method described in the specification of our copending patent application No. 81,11223, now published as British Application No. 2,096,502, filed Oct. 20, 1982. In accordance with that method the cylindrical assembly is bound with a refractory tape which shrinks on heating to a greater degree than the ceramic parts of the assembly. Thus on firing, the tape pulls the truncated wedges tightly together causing the side-faces of the spacers to provide good support for the walls of the mould. The ceramic moulds and cores in their green state have a degree of flexibility and, during the early part of the firing step, any distortions will be straightened out by the pressure from the spacers.
Where the mould is formed with an integral core, as described above, the graphite spacers will support the walls of the mould from inward distortion until the temperature is reached at which they burn out. If the mould is made without a core, however, it is preferable to provide support on the inside of the mould, and this can be done by filling the mould with a non-sintering ceramic powder, for example re-crystallised alumina 34, as shown in FIG. 7, or by supports positioned at different places within the mould cavity. In the latter case, the supports may conveniently be provided by embedding in the disposable pattern, pins made from a high temperature disposable material, for example, the graphite supported resin hereinbefore described. These will remain in place when the disposable material is removed but will burn out before the highest sintering temperature of the ceramic is reached.
Turning now to the materials to be used in the method described above, one of the advantages of the present invention is that it allows a much wider choice for the ceramic material of the mould than the lost wax process. Thus the ceramic material may be a conventional silica composition or one of the higher strength ceramics, such as alumina or zirconia may be used.
The ceramic material is mixed with a resin binder for the injection process. The binder may be a thermo-plastic resin which, on injection into a cold die, sets solid, but which softens again on heating. Using such resins the disposable pattern may be a conventional wax pattern.
In order to take advantage of the benefits of firing the ceramic in a cylindrical assembly, as described above, we prefer to use a thermo-setting resin, which is injected into a hot die and cured. Such resins once cured retain their strength during the early part of the firing process and do not soften again. Of course, a mixture of the two types of resin may be used provided adequate strength is maintained.
When using thermosetting resin binders, the disposable pattern material must be capable of withstanding the temperature and pressure during the injection of the ceramic material without deformation, but must be capable of being removed by a relatively simple process, for example, burning, melting or dissolution. A preferred material is a water soluble organic compound, for example, cane sugar which retains adequate strength to beyond 150° C., which is the usual injection temperature of the ceramic using a thermosetting resin binder.
The cane sugar contains an inert filler such as mica or slate powder, but preferably a soluble filler is used, for example, ammonium chloride and it may contain effervescing agents. Alternatively some low melting point metal alloys may be used, for example, those tin-zinc alloys sold under the Trade names of CERROBENT or CERROTRUE.
The chaplets 22 for supporting the pattern 16 in the die 20 must also withstand the pressure and temperature of the injection process. However, since these spacers span the space 24 into which the ceramic is injected, they are preferably made from the same material as the ceramic material being injected but which has previously been cured to its green state. We have found that during the injection process the ceramic integrates with the pieces of the same material cured to the green state to such an extend that the pieces become absorbed into a homogeneous mass without leaving any areas of weakness. These supports thus become part of the mould itself.
The core material need not be alumina but is selected in dependence on the requirements of the casting process. Thus silica or any other known core material may be used. However, another particular advantage of the invention is that the core and mould can be made from the same ceramic material in the same thermosetting resin binder. When injected hot, the binder cures to the green state which has intermediate strength and some flexibility. The mould with its core and supports can all be fired together at the same temperature and there will be no distortion due to differential thermal expansions or differential shrinkage. Thus the core remains accurately positioned within the final mould.
The high temperature chaplets 13 may, as an alternative to the graphite compound, be made from a metal compatible with that being cast, and which can be allowed to dissolve in the casting rather than being burned out as the graphite spacers are.
It will be appreciated that the above-described process enables a core to be accurately located in a mould which is itself made by a transfer moulding technique, so that none of the accuracy provided by the injection process of mould manufacture is lost.
One advantage of the above-described process over the conventional lost wax process is that the ceramic from which the mould is made can be accurately injected to give a very thin homogeneous wall thickness. This enables high heat conductivity to be achieved which speeds up the cooling process after casting. The homogeneous material is of uniform cross-section and is not subject to flaking or cracking as is the conventional invested shell mould. Because of the choice of materials available with this process, a material having the most beneficial combination of strength and thermal conductivity can be chosen depending on the casting process being used. Clearly the mould can have a varying wall thickness if desired.
In order to make a mould without a core, the process is simplified by the elimination of the first step. A disposable article is made without the core and is supported in a die as described above while ceramic is injected around it.
The mould described above may form part of a larger multiple mould assembly made completely by an injection process, thus eliminating the need for the time-consuming lost wax investment process currently used for making multiple moulds for casting aerofoil blades in the aero engine industry.
The mould shown in the example described above is open-ended ready for connection to a runner system in such a larger assembly. However, individual moulds with their own runner and riser systems can also be made by the method of the invention.

Claims (15)

I claim:
1. A method of making a seamless ceramic casting mould with a thin outer wall comprising the steps of:
making a first die, at least a part of which defines the shape of an article to be cast,
providing within the die one or more high temperature disposable supports which support the thin outer mould wall during the firing process but which are disposable at a temperature at which the thin outer mould wall has acquired self-supporting strength,
filling the die with a disposable pattern material whereby the supports become embedded in the pattern material, and allowing the pattern material to set,
removing the disposable pattern from the first die and inserting it into a second die, the inner surface of which is dimensioned to conform generally with the outer surface of at least the article-defining part of the pattern and to define a space therewith which conforms to the required thickness of the outer wall of the mould,
providing supports between the pattern and the die which are made from a ceramic material,
injecting a ceramic material under pressure into the space and allowing it to set to form the outer wall of the ceramic casting mould, the inner surface of such outer wall defining the outer surface of the article to be cast,
removing the disposable pattern from within the mould and firing the mould.
2. A method as claimed in claim 1 and wherein the step of firing the ceramic includes the additional steps of:
making an assembly of moulds in their pre-fired condition together with spacer members of generally truncated wedge shape placed alternately between them, the spacer members being made of a material having a shrinkage rate on heating which is compatible with that of the mould material,
holding the assembly tightly together in a cylindrical or polygonal array whereby the spacers provide support for the external walls of the moulds during firing, and
firing the assembly of moulds and spacers together.
3. A method as claimed in claim 2 and wherein the assembly is held together by means of a ceramic tape wound around it, and which shrinks at a greater rate than the materials of the ceramic and spacers on heating, whereby the array of moulds and spacers is pulled together to take up any shrinkage on heating.
4. A method as claimed in claim 1 and in which the step of injecting ceramic material into the die includes the further steps of mixing the ceramic material with a thermosetting resin binder, heating the die and injecting the ceramic material mixture into the heated die.
5. A method as claimed in claim 1 and in which the ceramic material is chosen from silica alumina or zirconia.
6. A method as claimed in claim 1 and in which the disposable material is a low melting point metal.
7. A method as claimed in claim 1 and in which the disposable material is a water soluble organic compound.
8. A method as claimed in claim 7 and in which the water soluble organic compound is cane sugar.
9. A method as claimed in claim 8 and in which the cane sugar includes a filler material.
10. A method as claimed in claim 1 and comprising the additional step of providing a core within the disposable material which remains in the mould when the disposable material is removed whereby hollow articles can be cast in the mould.
11. A method as claimed in claim 10 and wherein the core is provided by the steps of locating the core in a die, the internal surfaces of which define the shape of the article to be cast, but leaving end and edge portions of the core exposed, and injecting the disposable material into the die.
12. A method as claimed in claim 11 and in which the core is supported in the die by high temperature chaplets.
13. A method as claimed in claim 10 and in which the core is itself transfer mould and cured to its green state, the core being fired during the firing of the mould.
14. A method as claimed in claim 13 and in which the core is made from the same material as the mould.
15. A method of making a seamless ceramic casting mould with a thin outer wall comprising the steps of:
making a first die, at least a part of which defines the shape of an article to be cast,
filling the die with a disposable pattern material and allowing the pattern material to set,
removing the disposable pattern from the first die and inserting it into a second die, the inner surface of which is dimensioned to conform generally with the outer surface of at least the article-defining part of the pattern and to define a space therewith which conforms to the required thickness of the outer wall of the mould,
providing supports between the pattern and the die which are made from a ceramic material,
injecting a ceramic material under pressure into the space and allowing it to set to form the outer wall of the ceramic casting mould, the inner surface of such outer wall defining the outer surface of the article to be cast,
removing the disposable pattern from within the mould,
filling the hollow mould with a non-sintering ceramic powder to provide support for the inner surface of the outer mould wall during the firing step, and firing the mould.
US06/509,812 1982-07-03 1983-06-30 Ceramic casting mould and a method for its manufacture Expired - Fee Related US4617977A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB8219293 1982-07-03
GB8219293 1982-07-03

Publications (1)

Publication Number Publication Date
US4617977A true US4617977A (en) 1986-10-21

Family

ID=10531462

Family Applications (1)

Application Number Title Priority Date Filing Date
US06/509,812 Expired - Fee Related US4617977A (en) 1982-07-03 1983-06-30 Ceramic casting mould and a method for its manufacture

Country Status (4)

Country Link
US (1) US4617977A (en)
EP (1) EP0099215B1 (en)
JP (1) JPS5982142A (en)
DE (1) DE3371604D1 (en)

Cited By (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5069271A (en) * 1990-09-06 1991-12-03 Hitchiner Corporation Countergravity casting using particulate supported thin walled investment shell mold
US5248552A (en) * 1990-07-11 1993-09-28 Advanced Plastics Partnership Molding core
US5262100A (en) * 1990-07-11 1993-11-16 Advanced Plastics Partnership Method of core removal from molded products
US5295530A (en) * 1992-02-18 1994-03-22 General Motors Corporation Single-cast, high-temperature, thin wall structures and methods of making the same
US5297615A (en) * 1992-07-17 1994-03-29 Howmet Corporation Complaint investment casting mold and method
USRE35334E (en) * 1990-07-11 1996-09-24 Advanced Plastics Partnership Process for core removal from molded products
WO1999029451A1 (en) * 1997-12-08 1999-06-17 The Milwaukee School Of Engineering Method of using lost metal patterns to form ceramic molds
US6050325A (en) * 1998-09-16 2000-04-18 Pcc Airfoils, Inc. Method of casting a thin wall
US6119763A (en) * 1997-10-16 2000-09-19 Bridgestone Sports Co., Ltd. Method for preparing golf ball mold
WO2001015850A2 (en) * 1999-08-31 2001-03-08 Massachusetts Institute Of Technology Method and apparatus for encapsulating a workpiece which is to be machined
WO2001045877A2 (en) * 1999-10-26 2001-06-28 Howmet Research Corporation Multi-wall core and process
US6634410B1 (en) * 2001-08-28 2003-10-21 John H. Wilson Mold apparatus and method
US20060065383A1 (en) * 2004-09-24 2006-03-30 Honeywell International Inc. Rapid prototype casting
US20060175034A1 (en) * 2005-02-10 2006-08-10 Jorge Okhuysen-Caredenas Fluid-Soluble Pattern Material for Investment Casting Process, and Methods for Using Same
US20070003426A1 (en) * 2005-06-30 2007-01-04 Honeywell International, Inc. Advanced sintering process and tools for use in metal injection molding of large parts
US20080135202A1 (en) * 2006-12-06 2008-06-12 General Electric Company Composite core die, methods of manufacture thereof and articles manufactured therefrom
US8708029B2 (en) 2010-10-19 2014-04-29 Snecma Injection mold for a wax model of a turbine blade having an isostatic core holder
EP3019313A1 (en) * 2013-07-09 2016-05-18 United Technologies Corporation Ceramic-encapsulated thermopolymer pattern or support with metallic plating
RU176934U1 (en) * 2016-11-08 2018-02-02 Федеральное государственное бюджетное образовательное учреждение высшего образования "Комсомольский-на-Амуре государственный технический университет" (ФГБОУ ВО "КнАГТУ") DEVICE FOR ELECTROPHORESIS PRODUCTION OF SHELL CASES OF CERAMIC FORMS
US10927843B2 (en) 2013-07-09 2021-02-23 Raytheon Technologies Corporation Plated polymer compressor
US11267576B2 (en) 2013-07-09 2022-03-08 Raytheon Technologies Corporation Plated polymer nosecone
US11268526B2 (en) 2013-07-09 2022-03-08 Raytheon Technologies Corporation Plated polymer fan
US11691388B2 (en) 2013-07-09 2023-07-04 Raytheon Technologies Corporation Metal-encapsulated polymeric article

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS62227603A (en) * 1986-03-31 1987-10-06 日本碍子株式会社 Manufacture of ceramics sintered body and molding tool used for said manufacture
DE19726111C1 (en) * 1997-06-20 1998-11-12 Mtu Muenchen Gmbh Process for the production of a turbomachine blade by casting
GB0226559D0 (en) * 2002-11-14 2002-12-18 Rolls Royce Plc Investment moulding process and apparatus
CN117086264B (en) * 2023-10-19 2023-12-19 中北大学 Casting method combining frozen sand mold and gypsum mold

Citations (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2793412A (en) * 1950-12-15 1957-05-28 Gen Motors Corp Blade investment casting process
US2875485A (en) * 1953-12-17 1959-03-03 Sulzer Ag Precision casting mold and method of making the same
CA720301A (en) * 1965-10-26 Operhall Theodore Method of casting and element for use in same
GB1093726A (en) * 1964-12-10 1967-12-06 Plansee Metallwerk Improvements in and relating to permanent moulds for the casting of metals
GB1135255A (en) * 1965-10-21 1968-12-04 Participations Kali Ouest Soc Method and apparatus for the preparation of models used in casting
CA873723A (en) * 1971-06-22 R. Harm Alson Package for cylindrical articles or objects
US3596703A (en) * 1968-10-01 1971-08-03 Trw Inc Method of preventing core shift in casting articles
GB1346576A (en) * 1971-04-19 1974-02-13 Secr Defence Method of making a mould or mould piece
JPS5137820A (en) * 1974-09-28 1976-03-30 Kubota Ltd Chuzoyo shoshitsuseimokeizairyo
DE2651144A1 (en) * 1975-11-10 1977-05-26 Inst Odlewnictwa METHOD FOR MANUFACTURING MOLDED SHELLS OF CORES FROM THERMO-CARD LIQUID MASS AND DEVICE FOR CARRYING OUT THE METHOD
US4043379A (en) * 1976-04-12 1977-08-23 Trw Inc. Method of making a mold
US4066116A (en) * 1976-01-29 1978-01-03 Trw Inc. Mold assembly and method of making the same
US4068702A (en) * 1976-09-10 1978-01-17 United Technologies Corporation Method for positioning a strongback
US4108931A (en) * 1975-01-15 1978-08-22 Ralph Ogden System of making molds for investment casting
US4133371A (en) * 1976-08-31 1979-01-09 Rolls-Royce Limited Casting
DE2900959A1 (en) * 1978-01-13 1979-07-19 Trw Inc METHOD AND DEVICE FOR ASSEMBLING A CASTING FORM OR COCILLE
GB2028928A (en) * 1978-08-17 1980-03-12 Ross Royce Ltd Aerofoil blade for a gas turbine engine
GB2096502A (en) * 1981-04-09 1982-10-20 Rolls Royce Making refractory articles eg casting moulds and cases
GB2096503A (en) * 1981-04-13 1982-10-20 Rolls Royce Mould assembly for producing multiple castings

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5445314A (en) * 1977-09-16 1979-04-10 Kubota Ltd Method of making centerless ceramic core
JPS5475424A (en) * 1977-11-26 1979-06-16 Kawasaki Heavy Ind Ltd Extingish mold for pregision casting and method of casting same

Patent Citations (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA720301A (en) * 1965-10-26 Operhall Theodore Method of casting and element for use in same
CA873723A (en) * 1971-06-22 R. Harm Alson Package for cylindrical articles or objects
US2793412A (en) * 1950-12-15 1957-05-28 Gen Motors Corp Blade investment casting process
US2875485A (en) * 1953-12-17 1959-03-03 Sulzer Ag Precision casting mold and method of making the same
GB1093726A (en) * 1964-12-10 1967-12-06 Plansee Metallwerk Improvements in and relating to permanent moulds for the casting of metals
GB1135255A (en) * 1965-10-21 1968-12-04 Participations Kali Ouest Soc Method and apparatus for the preparation of models used in casting
US3596703A (en) * 1968-10-01 1971-08-03 Trw Inc Method of preventing core shift in casting articles
GB1346576A (en) * 1971-04-19 1974-02-13 Secr Defence Method of making a mould or mould piece
JPS5137820A (en) * 1974-09-28 1976-03-30 Kubota Ltd Chuzoyo shoshitsuseimokeizairyo
US4108931A (en) * 1975-01-15 1978-08-22 Ralph Ogden System of making molds for investment casting
DE2651144A1 (en) * 1975-11-10 1977-05-26 Inst Odlewnictwa METHOD FOR MANUFACTURING MOLDED SHELLS OF CORES FROM THERMO-CARD LIQUID MASS AND DEVICE FOR CARRYING OUT THE METHOD
US4129169A (en) * 1975-11-10 1978-12-12 Przedsicbiorstwo Projektowania I Realizacji Inwestycji Przemyslu Maszynowego "Bipromasz", Instytut Odlewnictwa Apparatus for making shells from thermosetting liquid compounds
US4066116A (en) * 1976-01-29 1978-01-03 Trw Inc. Mold assembly and method of making the same
US4043379A (en) * 1976-04-12 1977-08-23 Trw Inc. Method of making a mold
US4133371A (en) * 1976-08-31 1979-01-09 Rolls-Royce Limited Casting
GB1584367A (en) * 1976-08-31 1981-02-11 Rolls Royce Mould assembly for producing multiple castings
US4068702A (en) * 1976-09-10 1978-01-17 United Technologies Corporation Method for positioning a strongback
DE2900959A1 (en) * 1978-01-13 1979-07-19 Trw Inc METHOD AND DEVICE FOR ASSEMBLING A CASTING FORM OR COCILLE
GB2012640A (en) * 1978-01-13 1979-08-01 Trw Inc Method of assembling moulds
GB2028928A (en) * 1978-08-17 1980-03-12 Ross Royce Ltd Aerofoil blade for a gas turbine engine
US4421153A (en) * 1978-08-17 1983-12-20 Rolls-Royce Limited Method of making an aerofoil member for a gas turbine engine
GB2096502A (en) * 1981-04-09 1982-10-20 Rolls Royce Making refractory articles eg casting moulds and cases
GB2096503A (en) * 1981-04-13 1982-10-20 Rolls Royce Mould assembly for producing multiple castings

Cited By (34)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USRE35334E (en) * 1990-07-11 1996-09-24 Advanced Plastics Partnership Process for core removal from molded products
US5248552A (en) * 1990-07-11 1993-09-28 Advanced Plastics Partnership Molding core
US5262100A (en) * 1990-07-11 1993-11-16 Advanced Plastics Partnership Method of core removal from molded products
US5069271A (en) * 1990-09-06 1991-12-03 Hitchiner Corporation Countergravity casting using particulate supported thin walled investment shell mold
US5295530A (en) * 1992-02-18 1994-03-22 General Motors Corporation Single-cast, high-temperature, thin wall structures and methods of making the same
US5545003A (en) * 1992-02-18 1996-08-13 Allison Engine Company, Inc Single-cast, high-temperature thin wall gas turbine component
US6255000B1 (en) 1992-02-18 2001-07-03 Allison Engine Company, Inc. Single-cast, high-temperature, thin wall structures
US5297615A (en) * 1992-07-17 1994-03-29 Howmet Corporation Complaint investment casting mold and method
US6119763A (en) * 1997-10-16 2000-09-19 Bridgestone Sports Co., Ltd. Method for preparing golf ball mold
WO1999029451A1 (en) * 1997-12-08 1999-06-17 The Milwaukee School Of Engineering Method of using lost metal patterns to form ceramic molds
US6050325A (en) * 1998-09-16 2000-04-18 Pcc Airfoils, Inc. Method of casting a thin wall
WO2001015850A2 (en) * 1999-08-31 2001-03-08 Massachusetts Institute Of Technology Method and apparatus for encapsulating a workpiece which is to be machined
WO2001015850A3 (en) * 1999-08-31 2001-06-21 Massachusetts Inst Technology Method and apparatus for encapsulating a workpiece which is to be machined
US6688871B1 (en) 1999-08-31 2004-02-10 Massachusetts Institute Of Technology Apparatus for encapsulating a workpiece which is to be machined
WO2001045877A3 (en) * 1999-10-26 2003-11-06 Howmet Res Corp Multi-wall core and process
US6626230B1 (en) 1999-10-26 2003-09-30 Howmet Research Corporation Multi-wall core and process
WO2001045877A2 (en) * 1999-10-26 2001-06-28 Howmet Research Corporation Multi-wall core and process
US6634410B1 (en) * 2001-08-28 2003-10-21 John H. Wilson Mold apparatus and method
US7448433B2 (en) * 2004-09-24 2008-11-11 Honeywell International Inc. Rapid prototype casting
US20060065383A1 (en) * 2004-09-24 2006-03-30 Honeywell International Inc. Rapid prototype casting
US20060175034A1 (en) * 2005-02-10 2006-08-10 Jorge Okhuysen-Caredenas Fluid-Soluble Pattern Material for Investment Casting Process, and Methods for Using Same
US20070003426A1 (en) * 2005-06-30 2007-01-04 Honeywell International, Inc. Advanced sintering process and tools for use in metal injection molding of large parts
US7413702B2 (en) 2005-06-30 2008-08-19 Honeywell International Inc. Advanced sintering process and tools for use in metal injection molding of large parts
US9566642B2 (en) 2006-12-06 2017-02-14 General Electric Company Composite core die, methods of manufacture thereof and articles manufactured therefrom
US8413709B2 (en) * 2006-12-06 2013-04-09 General Electric Company Composite core die, methods of manufacture thereof and articles manufactured therefrom
US20080135202A1 (en) * 2006-12-06 2008-06-12 General Electric Company Composite core die, methods of manufacture thereof and articles manufactured therefrom
US8708029B2 (en) 2010-10-19 2014-04-29 Snecma Injection mold for a wax model of a turbine blade having an isostatic core holder
EP3019313A1 (en) * 2013-07-09 2016-05-18 United Technologies Corporation Ceramic-encapsulated thermopolymer pattern or support with metallic plating
EP3019313A4 (en) * 2013-07-09 2017-04-05 United Technologies Corporation Ceramic-encapsulated thermopolymer pattern or support with metallic plating
US10927843B2 (en) 2013-07-09 2021-02-23 Raytheon Technologies Corporation Plated polymer compressor
US11267576B2 (en) 2013-07-09 2022-03-08 Raytheon Technologies Corporation Plated polymer nosecone
US11268526B2 (en) 2013-07-09 2022-03-08 Raytheon Technologies Corporation Plated polymer fan
US11691388B2 (en) 2013-07-09 2023-07-04 Raytheon Technologies Corporation Metal-encapsulated polymeric article
RU176934U1 (en) * 2016-11-08 2018-02-02 Федеральное государственное бюджетное образовательное учреждение высшего образования "Комсомольский-на-Амуре государственный технический университет" (ФГБОУ ВО "КнАГТУ") DEVICE FOR ELECTROPHORESIS PRODUCTION OF SHELL CASES OF CERAMIC FORMS

Also Published As

Publication number Publication date
JPS5982142A (en) 1984-05-12
EP0099215B1 (en) 1987-05-20
DE3371604D1 (en) 1987-06-25
EP0099215A1 (en) 1984-01-25

Similar Documents

Publication Publication Date Title
US4617977A (en) Ceramic casting mould and a method for its manufacture
US6626230B1 (en) Multi-wall core and process
US4434835A (en) Method of making a blade aerofoil for a gas turbine engine
JP4344787B2 (en) Ceramic core with internal reinforcement
CA1064220A (en) Investment casting mold and process
US4384607A (en) Method of manufacturing a blade or vane for a gas turbine engine
US6186217B1 (en) Multipiece core assembly
WO2000078480A1 (en) Multipiece core assembly for cast airfoil
US4552197A (en) Mould assembly for casting metal articles and a method of manufacture thereof
US6298899B1 (en) Water jacket core
US5623985A (en) Apparatus and method for molding an article
US4520117A (en) Refractory articles and the method for the manufacture thereof
US3320345A (en) Method for the production of cored patterns
GB2090181A (en) Manufacturing a Blade or Vane for a Gas Turbine Engine
US6349759B1 (en) Apparatus and method for casting a metal article
JP3133407B2 (en) Manufacturing method of ceramic mold
US3722577A (en) Expansible shell mold with refractory slip cover and the method of making same
JPH0323036A (en) Assembled sand core for high pressure casting
JP3552298B2 (en) Mold for hot impeller casting
JPH0813400B2 (en) Precision casting method for castings having a narrow hollow portion
JPS61222659A (en) Molding method for wax pattern in lost wax casting method
JPS6359787B2 (en)
GB1605341A (en) Improvements in investment casings of moulds
JPH04189101A (en) Integral molding method of heat exchanger body made of ceramics
JPH07214235A (en) Production of casting mold for precision casting

Legal Events

Date Code Title Description
AS Assignment

Owner name: ROLLS-ROYCE LIMITED, 65 BUCKINGHAM GATE, LONDON SW

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST.;ASSIGNOR:MILLS, DAVID;REEL/FRAME:004206/0343

Effective date: 19830627

FEPP Fee payment procedure

Free format text: PAYOR NUMBER ASSIGNED (ORIGINAL EVENT CODE: ASPN); ENTITY STATUS OF PATENT OWNER: LARGE ENTITY

FPAY Fee payment

Year of fee payment: 4

REMI Maintenance fee reminder mailed
LAPS Lapse for failure to pay maintenance fees
FP Lapsed due to failure to pay maintenance fee

Effective date: 19941026

STCH Information on status: patent discontinuation

Free format text: PATENT EXPIRED DUE TO NONPAYMENT OF MAINTENANCE FEES UNDER 37 CFR 1.362